Moments of Inertia of Several Airplanes

Moments of Inertia of Several Airplanes

Author: Marvel P. Miller

Publisher:

Published: 1931

Total Pages: 10

ISBN-13:

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The National Advisory Committee for Aeronautics has adopted the practice of measuring the moments of inertia of all airplanes that become available through their use in flight research work. This paper, which is the first of a series presenting the results of such measurements, gives the momumental ellipsoids of ten army and naval biplanes and one commercial monoplane. The data wer obtained by the use of a pendulum method, previously described. The moments of inertia are expressed in coeffienct as well as in dimensional form, so that those for airplanes of widely spaced different weights and dimensions can be compared. The coefficients are also useful for estimating the moments of inertia of airplanes for which no measurements of inertia can be computed. To determine the accuracy with which the moments of inertia can be computed from design data, calculations were made of the monents of inertia for one of the above airplanes by summing up the moments of inertia of its constituent parts. It was found that computed values were in error 20, 10, and 5 percent for the X, Y, and Z axes, respectively.


An Accurate Method of Measuring the Moments of Inertia of Airplanes

An Accurate Method of Measuring the Moments of Inertia of Airplanes

Author: M. P. Miller

Publisher:

Published: 1930

Total Pages: 606

ISBN-13:

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This note contains a description of an improved apparatus and procedure used for determining the moments of inertia of airplanes. The method, based on the pendulum theory, is similar to that previously used, but a recent investigation of its accuracy has resulted in the improvements described herein. The error, when using the new apparatus and procedure, has been found to be of the order of 1 percent. Sample data and calculation for an airplane are included in an appendix.


Measurement of the Longitudinal Moment of Inertia of a Flexible Airplane

Measurement of the Longitudinal Moment of Inertia of a Flexible Airplane

Author: Henry A. Cole

Publisher:

Published: 1956

Total Pages: 40

ISBN-13:

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The application and results of the above method in ground oscillation tests are described. The various corrections to reduce the measured moment of inertia to the reference axis moment of inertia are presented. The results show that measurement of moment of inertia by this method is practicable, provided the knife edges and spring are arranged to minimize excitation of structural modes.


Report

Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1937

Total Pages: 28

ISBN-13:

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Notes on the Stalling of Vertical Tail Surfaces and on Fin Design

Notes on the Stalling of Vertical Tail Surfaces and on Fin Design

Author: F. L. Thompson

Publisher:

Published: 1940

Total Pages: 566

ISBN-13:

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It may be concluded that the stalling of vertical tail surfaces is not in itself a dangerous condition. Provided sufficient directional stability exists at large angles of sideslip, the tail stall may occur with modern airplanes, as with those of the past, without the knowledge of or concern to the pilot.